Intermix combustion chamber of NASA JX-2 Engine
thingiverse
This scale model showcases the combustion chamber of a J-2X liquid-fuel cryogenic rocket engine, slated for use in NASA's Constellation program and Space Launch System. The J-2X powers up by burning cryogenic liquid hydrogen & liquid oxygen propellants, resulting in 1,307 kN (294,000 lbf) of thrust in vacuum with a specific impulse of 448 seconds (4.39 km/s). With a mass of approximately 5,450 pounds (2,470 kg), this engine is notably heavier than its predecessors used in the Saturn 5. Engineers and educators alike will find this model particularly fascinating. Visit our site http://www.creationengineering.co.uk for more information on our technology, research, and groundbreaking innovations. Keep up to date with our latest developments by following us on Twitter @bioprinting2.
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